• Title/Summary/Keyword: Aircraft safety

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Study on the Application of Airworthiness Standard for the e-VTOL (e-VTOL 항공기의 감항기술기준 적용 연구)

  • Choi, Joo-Won;Hwang, Chang-Jeon;Suk, Jin-Young
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.7
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    • pp.593-599
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    • 2021
  • The demand for e-VTOL aircraft is expected to be increased rapidly in the future as a means of urban transportation due to operating cost reduction, eco-friendliness and convenience of vertical take-off and landing using pilot-aids automation system. However, there are many technical hurdles to be solved in securing safety and certification which are essential for commercialization and urban operation. So far, there is no e-VTOL aircraft that has received type certificate and standard airworthiness certificate due to the technical problems and safety requirement differences with conventional aircraft. The e-VTOL aircraft certification should also meet the equivalent level of safety required by the current airworthiness standards, but there are existing problems in securing safety and meeting current standards. In this study, the e-VTOL's certification problems and technical limitations in satisfying the current standards are presented.

Computational Simulation of Lightning Strike on Aircraft and Design of Lightning Protection System (항공기 낙뢰 전산 시뮬레이션 및 보호시스템 설계)

  • Kim, Jong-Jun;Baek, Sang-Tae;Song, Dong-Geon;Myong, Rho-Shin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.12
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    • pp.1071-1086
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    • 2016
  • The safety of aircraft can be threatened by environmental factors, such as icing, turbulence, and lightning strike. Due to its adverse effects on aircraft structure and electronic components of aircraft, lightning strike is one of the biggest hazards on aircraft safety. Lightning strike can inject high voltage electric current to the aircraft, which may generate strong magnetic field and extreme hot spots, leading to severe damage of structure or other equipment in aircraft. In this work, mechanism of lightning strike and associated direct and indirect effects of lightning on aircraft were studied. First, on the basis of aircraft lightning regulations provided by Aerospace Recommended Practice (ARP), we considered different lightning waveform and zones of an aircraft. A coupled thermal-electrical computational model of ABAQUS was then used for simulating flow of heat and electric current caused by a lightning strike. A study on fuel tank, with and without lightning protection system, was also conducted using the computational model. Finally, electric current flow on two full scale airframes was analyzed using the EMA3D code.

A Study for Improvements on Aircraft mechanic Certification System and mechanics education (항공정비사 자격증명 제도개선 및 교육기관 선진화 방안 연구)

  • Park, Hak-Sun;Lee, Su-Mi;Lee, Myeong-U;Lee, Jong-Seo
    • 한국항공운항학회:학술대회논문집
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    • 2016.05a
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    • pp.162-177
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    • 2016
  • The government conducted an aviation expert training project in 2013. But unfortunately, only pilots and international experts were targeted and aircraft maintenance engineers that are the most important to safety were not trainee to the training courses. More importantly, the more the absolute number of aircrafts increases, the more demand for aircraft maintenance engineers are going up as well. Through the evaluation indicators for the Government-Sponsored Program Fostering Aviation Personnel(aircraft maintenance engineers). it figured out factors associated with the Government-Sponsored Program Fostering Aircraft Maintenance Engineers and it suggested a baseline data necessary to inspect and manage professional training institutions. Thanks to the development of the evaluation indicators, it is highly expected that difference among institutions will be narrowed, elevated level of management of the institutions will help foster and yield satisfactory aircraft maintenance engineers.

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Effects of different roll angles on civil aircraft fuselage crashworthiness

  • Mou, Haolei;Du, Yuejuan;Zou, Tianchun
    • Advances in aircraft and spacecraft science
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    • v.2 no.4
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    • pp.391-401
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    • 2015
  • Crashworthiness design and certification have been and will continue to be the main concern in aviation safety. The effects of roll angles on fuselage section crashworthiness for typical civil transport category aircrafts were investigated. A fuselage section with waved-plates under cargo floor is suggested, and the finite element model of fuselage section is developed to simulate drop test subjected to 7 m/s impact velocity under conditions of 0-deg, 5-deg, 10-deg and 15-deg roll angles, respectively. A comparative analysis of failure modes, acceleration responses, and energy absorption of fuselage section under various conditions are given. The results show that the change of roll angles will significantly affect fuselage deformation, seat peak overloads, and energy absorption. The crashworthiness capability of aircraft can be effectively improved by choosing appropriate landing way.

Accident Analysis & Lessons Learned of B737MAX JT610 from a Flight Control System Design Perspective (비행제어시스템 설계 관점의 B737MAX JT610편 사고분석과 교훈)

  • Moon, Jung-Ho;Cho, Hwankee
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.28 no.1
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    • pp.106-114
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    • 2020
  • The Lion Air JT610 accident in Indonesia in October 2018, along with the Ethiopian Airline ET302 accident in March 2019, is an significant aircraft accident that detects defects of the B737MAX aircraft. Shortly after the accident, the FAA prohibited operation of the aircraft. This action has affected the market environment of airlines and aircraft manufacturers around the world. In October 2019, Indonesian Traffic Safety Committee released an accident investigation report for Lion Air JT610, which concluded that the causes of the accident were MCAS design defects, lack of education and training, and errors in the repair process. This paper summarizes the flight control system of the B737MAX aircraft, the causes of the accident based on the final accident investigation report, and provides considerations for aircraft design and retrofit.

A Development of 3-D Resolution Algorithm for Aircraft Collision Avoidance

  • Kim, Youngrae;Lee, Sangchul;Lee, Keumjin;Kang, Ja-Young
    • International Journal of Aeronautical and Space Sciences
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    • v.14 no.3
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    • pp.272-281
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    • 2013
  • Traffic Collision Avoidance System (TCAS) is designed to enhance safety in aircraft operations, by reducing the incidences of mid-air collision between aircraft. The current version of TCAS provides only vertical resolution advisory to the pilots, if an aircraft's collision with another is predicted to be imminent, while efforts to include horizontal resolution advisory have been made, as well. This paper introduces a collision resolution algorithm, which includes both vertical and horizontal avoidance maneuvers of aircraft. Also, the paper compares between the performance of the proposed algorithm and that of algorithms with only vertical or horizontal avoidance maneuver of aircraft.

Study for Certification of Aircraft De-icing System (항공기 제빙 시스템의 인증에 대한 연구)

  • Jun, Jonghyub
    • Journal of Aerospace System Engineering
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    • v.6 no.2
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    • pp.7-12
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    • 2012
  • De-icing system is essential for any aircraft to fly in icing conditions. So there are two kinds of aircraft-those that are certificated for flight in icing conditions and those that are not. Icing certification involves a rigorous testing program, and relatively few light aircraft carry this approval. From a legal perspective, aircraft that do not have all required ice protection equipment installed and functional are prohibited from venturing into an area where icing conditions are known. There are a few kinds of de-icing system. It is necessary to review the systems in point of aircraft certification considering the operational and safety issues.

Study on Evaluation of Structural Integrity for Small Aircraft Tail (소형 항공기 미익부 구조 건전성 평가에 관한 연구)

  • Lee, Muhyoung;Park, Illkyung;Kim, Sungjoon;Ahn, Sukmin
    • Journal of Aerospace System Engineering
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    • v.6 no.2
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    • pp.28-34
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    • 2012
  • Structural integrity evaluation is important item in the aircraft certification. Recently, it is designed for limit load, material weakness about fatigue and corrosion, damage by bird strike in flight to evaluate structural integrity of aircraft. And static/fatigue analysis are performed to secure structural integrity, it was verified by static and fatigue tests. To evaluate the structural integrity of small aircraft tail, structural integrity was calculated by the finite element analysis. In the present study, finite element analysis are performed to pick out load cases in flight occurrence, and secure margin of safety to evaluate structural integrity of KC-100 tail unit. The proprieties of finite element analysis results are compared with the static structure test results. The estimation process of structural integrity for small aircraft tail may help the design.

The Effect of Rapport on the Airplane on Reliability and Safety - Under the Pandemic - (기내에서의 라포가 신뢰성과 안전성에 미치는 영향 - 팬데믹 상황을 기반으로 -)

  • Kim, Kyoung Eun;Jeon, Seung Joon;Jung, Yun Sick
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.30 no.3
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    • pp.65-75
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    • 2022
  • This study tried to confirm whether the public's negative emotions such as fear and anxiety about corona virus infection caused by the spatial nature of the aircraft were alleviated due to factors of in-flight services focusing on hygiene and quarantine and further had a positive effect on the formation of Rapport between cabin crews and passengers. We also investigated the impact on passengers' perceptions such as Reliability and Safety which can be viewed as a new measure and standard of customer satisfaction in the Pandemic era through Rapport. A survey was conducted online in December 2021 for passengers with experience in boarding aircraft after the COVID-19 outbreak, and a total of 211 responses were used for analysis. As a result of the analysis of the data, it was confirmed that aircraft in-flight service had a positive (+) effect on Rapport, and Rapport between passengers and cabin crews had a positive (+) effect on passenger Reliability and Safety.

A Study on the Certification Method for the Application of Composite Material of eVTOL Aircraft (전기동력 수직이착륙 항공기의 복합재료 적용을 위한 소재인증 방안 고찰)

  • Bae, Sung-Hwan;Cho, Sung-In;Choi, Cheong-Ho;Jeon, Seungmok
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.12
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    • pp.969-976
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    • 2020
  • Urban Air Mobility is attracting attention as a future innovation industry around the world, and leading industries are considering the application of composite materials for structural robustness and lightening in the designing and manufacturing new concept eVTOL aircraft. To apply composite materials to the new concept of eVTO aircraft, this paper was analyzed about composite material qualification system of FAA & EASA and institutionalized by Korea Government, including the procedures and methods, the organization to carry out the material verification for domestic conditions. The domestic composite material qualification system will not only make it easier for manufacturers of eVTOL aircraft with a new concept to apply composite materials to domestic aircraft through pre-material qualification, but also reduce the burden of material qualification within the period of type certification. In addition, domestic manufacturers of composite materials with qualified material quality and performance will be easy to enter for domestic aircraft applications and composite material manufacturers with experience in applying to aircraft will have a positive impact on overseas exports. This system will be able to promote the development eVTOL aircraft industry of a new concept and enhance international credibility of made aircraft in Korea.